EP2435780A1 - Method for producing a large-calibre explosive projectile, and an explosive projectile produced using this method - Google Patents
Method for producing a large-calibre explosive projectile, and an explosive projectile produced using this methodInfo
- Publication number
- EP2435780A1 EP2435780A1 EP10720128A EP10720128A EP2435780A1 EP 2435780 A1 EP2435780 A1 EP 2435780A1 EP 10720128 A EP10720128 A EP 10720128A EP 10720128 A EP10720128 A EP 10720128A EP 2435780 A1 EP2435780 A1 EP 2435780A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- projectile casing
- projectile
- explosive
- explosive charge
- casing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000002360 explosive Substances 0.000 title claims abstract description 57
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 6
- 238000000034 method Methods 0.000 title claims description 10
- 239000004429 Calibre Substances 0.000 title abstract 2
- 239000013013 elastic material Substances 0.000 claims description 3
- 239000006260 foam Substances 0.000 claims description 3
- 239000000853 adhesive Substances 0.000 claims description 2
- 230000001070 adhesive effect Effects 0.000 claims description 2
- 238000003754 machining Methods 0.000 description 2
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
- F42B33/02—Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges
- F42B33/0207—Processes for loading or filling propulsive or explosive charges in containers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/207—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by the explosive material or the construction of the high explosive warhead, e.g. insensitive ammunition
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B30/00—Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
- F42B30/08—Ordnance projectiles or missiles, e.g. shells
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
- F42B33/001—Devices or processes for assembling ammunition, cartridges or cartridge elements from parts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
- F42B33/02—Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges
- F42B33/0214—Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges by casting
Definitions
- the invention relates to a method for producing a large-caliber explosive projectile with a projectile casing with ogivalem front part, which encloses a filled with a plastic-bonded explosive charge interior and has a tip side closable with a head detonator mouth hole.
- the invention further relates to a produced by this method large-caliber explosive projectile.
- Such a method is known, for example, from the document EP 1 338 860 B1.
- an existing example of an elastic plastic shell (hereinafter referred to as a liner) is introduced through the mouth hole in the interior of the projectile casing and then poured the explosive charge in the liner.
- the liner is required in this case to decouple the explosive charge to the inner wall of the projectile casing due to the different volumetric expansion coefficients of the explosive charge and the bullet casing material with temperature fluctuations.
- a disadvantage of the known method is especially that the mouth hole designed for screwing a detonator has a small diameter, so that both the introduction and positioning of the liner in the interior of the projectile casing as well as the introduction of the usually highly viscous castable explosive charge in the liner extraordinarily time consuming.
- the invention has for its object to provide a method of the type mentioned, in which both the liner and the explosive charge in a simple manner, quickly and accurately in the projectile casing of the projectile can be introduced. Except- this is to be disclosed a large-caliber explosive projectile, which is produced by this method.
- the invention is based essentially on the idea not to introduce the liner and the explosive charge through the designed for the head detonator mouth hole in the interior of the projectile casing, but by a much larger opening.
- the projectile casing is produced as an at least two-part casing, such that in the direction of the longitudinal axis of the projectile casing there is a rear-side projectile casing section and a ring-shaped, front projectile casing section containing the mouth-hole, wherein the two projectile casing sections in the region of the ogival front part preferably together via a screw connection are connectable.
- a liner adapted to the inner contour of the inner space and consisting of an elastic material is first introduced and positioned into the interior of the rear-side projectile casing section through its front opening. Then the plastic-bonded explosive charge is introduced into the liner, and after its curing, the liner is closed with a plastic, for example, existing lid. Subsequently, an elastic compensation element adapted to the internal geometry of the front-side projectile casing section is positioned on the cover and the two projectile casing sections are screwed together.
- the liner Due to the large opening of the rear-side projectile casing section, the liner can be easily creased and without further processing steps into the interior of this machine. Insert shell section and position it accurately.
- the also correspondingly large interpretable opening of the plastic cover allows a very good filling of the liner with the explosive charge, which can thus be filled voids and bubbles in the liner.
- the liner is selected so that the explosive charge protrudes from the front side over the rear-side projectile casing section, and that after curing of the explosive charge by appropriate processing the front ends with a flat surface and after connecting the two bullet casing sections in the interior of the front Projectile casing section protrudes.
- the liner is hermetically sealed by the lid and an applied seal.
- the length of the front projectile casing section is approximately equal to 1/3 of the total length of the projectile casing.
- the compensation element should preferably consist of an open-cell foam.
- the screw connection of the two projectile casing sections should preferably be secured against loosening by means of an adhesive.
- Fig. 1 shows the longitudinal section through an inventive explosive projectile
- FIG. 2 shows an enlarged view of the area designated by Il in FIG.
- 1 designates a large-caliber, spin-stabilized explosive projectile, as can be fired, for example, from a tank howitzer.
- the explosive projectile 1 comprises a projectile casing 2 with ogivalem front part 2 ' , a bottom part 3 and a front-side head detonator 4.
- the head detonator 4 is screwed into a tip-side arranged in the projectile casing 2 mouth hole 5.
- the projectile casing 2 surrounds an inner space 6, with the inner walls 7, an elastic plastic cover (liner) 8 is glued.
- liner 8 In the liner 8 is a plastic-bound, insensitive explosive charge 9.
- the explosive charge 9 is closed by an elastic compensating element 10, on whose side facing away from the explosive charge 9, the front region of the inner wall of the projectile casing 2 and the head igniter 4 exert a predeterminable pressure, so that the explosive charge 9 is under prestress.
- the projectile casing 2 viewed in the direction of its longitudinal axis 11, consists of two projectile casing sections 20, 21, which are connected to one another in the region of the ogival front section 2 ' by means of a screw connection 22 and secured against loosening by means of gluing.
- the liner 8 is then pushed and positioned by the relatively large opening 23 of the rear-side projectile casing section 20 into the interior 6 of this casing section.
- the length of the liner 8 is selected such that the liner 8 extends on the front side in front of the front edge 24 of the rear-side projectile casing section 20.
- the explosive charge 9 is then poured into the liner 8, such that the explosive charge 9 protrudes on the front side over the rear-side projectile casing section 20.
- the liner 8 After curing of the explosive charge 9, this is processed for example by means of a machining process such that the explosive charge 9 ends on the front side with a flat surface 25.
- the liner 8 is then provided with a cover 26 made of plastic and hermetically sealed by means of a bond.
- the exactly adapted to the internal geometry of the front floor shell portion 21 compensating element 10 is positioned from an open-cell foam.
- This compensating element 10 has a large footprint to the lid 26 of the liner 8.
- an explosive head detonator 4 is screwed into the mouth hole 5 and glued.
- the head detonator 4 can be designed such that it can be used for further compression of the compensating element 10.
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102009022495A DE102009022495A1 (en) | 2009-05-25 | 2009-05-25 | Method for producing a large-caliber explosive projectile and explosive projectile, produced by this method |
PCT/EP2010/002795 WO2010145734A1 (en) | 2009-05-25 | 2010-05-06 | Method for producing a large-calibre explosive projectile, and an explosive projectile produced using this method |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2435780A1 true EP2435780A1 (en) | 2012-04-04 |
EP2435780B1 EP2435780B1 (en) | 2013-07-10 |
Family
ID=42314825
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP10720128.7A Not-in-force EP2435780B1 (en) | 2009-05-25 | 2010-05-06 | Method for producing a large-calibre explosive projectile, and an explosive projectile produced using this method |
Country Status (6)
Country | Link |
---|---|
US (2) | US8601950B2 (en) |
EP (1) | EP2435780B1 (en) |
DE (1) | DE102009022495A1 (en) |
IL (1) | IL216499A (en) |
WO (1) | WO2010145734A1 (en) |
ZA (1) | ZA201107921B (en) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102009022495A1 (en) * | 2009-05-25 | 2010-12-02 | Rheinmetall Waffe Munition Gmbh | Method for producing a large-caliber explosive projectile and explosive projectile, produced by this method |
DE102012000011A1 (en) | 2012-01-02 | 2013-07-04 | Rheinmetall Waffe Munition Gmbh | Spin-stabilized explosive projectile |
EP3036497B1 (en) | 2013-08-20 | 2018-04-25 | BAE Systems PLC | Illumination munition |
US9797698B2 (en) * | 2013-08-20 | 2017-10-24 | Bae Systems Plc | Common carrier munition |
AU2014310467B2 (en) * | 2013-08-20 | 2017-10-12 | Bae Systems Plc | Frangible munition |
EP3036498B1 (en) | 2013-08-20 | 2017-06-07 | BAE Systems PLC | Smoke payload apparatus |
DE102013014665B3 (en) * | 2013-08-29 | 2014-04-30 | Bundesrepublik Deutschland, vertreten durch das BMVg, vertreten durch das Bundesamt für Ausrüstung, Informationstechnik und Nutzung der Bundeswehr | Explosive projectile has auger that is inserted into the explosive charge in the direction of the projectile axis, and head igniter that is fixed with auger |
ITBS20130145A1 (en) * | 2013-10-16 | 2015-04-17 | Rwm Italia S P A | METHOD OF LOADING AN EXPLOSIVE DEVICE WITH CONTROLLED DESTRUCTIVE CAPACITY AND ITS EXPLOSIVE DEVICE |
DE102013021030A1 (en) | 2013-12-17 | 2015-06-18 | Rheinmetall Waffe Munition Gmbh | Warhead and explosive charge module for such a warhead |
DE102014103105B3 (en) * | 2014-03-07 | 2014-12-04 | Rheinmetall Waffe Munition Gmbh | Method and production of a large caliber warhead and warhead produced by this method |
RU2576719C1 (en) * | 2015-03-10 | 2016-03-10 | Открытое акционерное общество "Центральный научно-исследовательский институт точного машиностроения" (ОАО "ЦНИИТОЧМАШ") | Artillery shells with unitary loading |
EP3091329B1 (en) | 2015-05-08 | 2017-12-27 | Diehl Defence GmbH & Co. KG | Method for producing a load for an explosive projectile |
DE102015005980A1 (en) | 2015-05-08 | 2016-11-10 | Diehl Bgt Defence Gmbh & Co. Kg | Explosive charge with vogegebenem volume and given outer shape and bullet |
DE102016008391B4 (en) * | 2016-07-09 | 2018-05-24 | Diehl Defence Gmbh & Co. Kg | bullet |
RU175283U1 (en) * | 2017-08-08 | 2017-11-29 | Федеральное государственное унитарное предприятие "Российский Федеральный ядерный центр - Всероссийский научно-исследовательский институт экспериментальной физики" (ФГУП "РФЯЦ-ВНИИЭФ") | Explosive device |
DE102018108766A1 (en) | 2018-04-12 | 2019-10-17 | Rheinmetall Waffe Munition Gmbh | explosive projectile |
DE102020116228B3 (en) | 2020-06-19 | 2021-12-23 | Rheinmetall Waffe Munition Gmbh | Bullet and ammunition |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2373883A (en) * | 1942-10-30 | 1945-04-17 | Clyde B Ferrel | Shell structure |
DE1024406B (en) | 1954-04-22 | 1958-02-13 | Guenther Voss Dr Ing | Twist-stabilized long bullet |
US3786714A (en) | 1970-11-02 | 1974-01-22 | Robertson Co H H | Military bomb and method of making same |
US3693548A (en) * | 1970-11-02 | 1972-09-26 | Robertson Co H H | Military bomb |
US4365556A (en) * | 1980-10-06 | 1982-12-28 | The United States Of America As Represented By The Secretary Of The Army | Method and system for preventing base separation of cast explosives in projectiles |
US4615272A (en) * | 1984-09-12 | 1986-10-07 | The United States Of America As Represented By The Secretary Of The Air Force | Bomb and bomb liner |
US5054399A (en) * | 1988-07-05 | 1991-10-08 | The United States Of America As Represented By The Secretary Of The Air Force | Bomb or ordnance with internal shock attenuation barrier |
US5939662A (en) * | 1997-12-03 | 1999-08-17 | Raytheon Company | Missile warhead design |
DE10207209A1 (en) | 2002-02-21 | 2003-09-11 | Rheinmetall W & M Gmbh | Process for producing a large-caliber explosive projectile and an explosive projectile produced by this process |
GB0205565D0 (en) * | 2002-03-11 | 2002-04-24 | Bae Systems Plc | Explosives liner |
DE10221759B4 (en) | 2002-05-16 | 2005-03-31 | Diehl Munitionssysteme Gmbh & Co. Kg | warhead |
DE102006034891A1 (en) * | 2006-07-25 | 2008-02-07 | Rheinmetall Waffe Munition Gmbh | liner |
US7992498B2 (en) * | 2006-08-25 | 2011-08-09 | Ruhlman James D | Reduced collateral damage bomb (RCDB) and system and method of making same |
DE102009022495A1 (en) * | 2009-05-25 | 2010-12-02 | Rheinmetall Waffe Munition Gmbh | Method for producing a large-caliber explosive projectile and explosive projectile, produced by this method |
-
2009
- 2009-05-25 DE DE102009022495A patent/DE102009022495A1/en not_active Withdrawn
-
2010
- 2010-05-06 US US13/322,510 patent/US8601950B2/en not_active Expired - Fee Related
- 2010-05-06 EP EP10720128.7A patent/EP2435780B1/en not_active Not-in-force
- 2010-05-06 WO PCT/EP2010/002795 patent/WO2010145734A1/en active Application Filing
-
2011
- 2011-10-28 ZA ZA2011/07921A patent/ZA201107921B/en unknown
- 2011-11-21 IL IL216499A patent/IL216499A/en not_active IP Right Cessation
-
2013
- 2013-10-31 US US14/068,783 patent/US8739671B2/en not_active Expired - Fee Related
Non-Patent Citations (1)
Title |
---|
See references of WO2010145734A1 * |
Also Published As
Publication number | Publication date |
---|---|
IL216499A (en) | 2015-07-30 |
US8739671B2 (en) | 2014-06-03 |
DE102009022495A1 (en) | 2010-12-02 |
ZA201107921B (en) | 2012-07-25 |
US8601950B2 (en) | 2013-12-10 |
EP2435780B1 (en) | 2013-07-10 |
US20140076129A1 (en) | 2014-03-20 |
WO2010145734A1 (en) | 2010-12-23 |
IL216499A0 (en) | 2012-01-31 |
US20120137918A1 (en) | 2012-06-07 |
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